Free Surface Impinging Jet

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F'''Heat transfer under free surfaceimpinging jet – Falkner-Skansimilaritysolution2{ } = 02⎤ ''⎡εdU ⎤'( Uξ) FF + 1−( )⎡εd+ ⎢ ⎥ ⎢ ⎥ F⎣νdx ⎦ ⎣ ν dx ⎦ε dν dx( Uε) = α2ε dUν dx=βThe Falkner-Skan similarity solution with β= 1 underlines the laminarboundary layer flow and heat transfer in the stagnation region, which hasbeen used to date.Using potential flow theory, Schlichting (1968) showed that the free streamvelocity at the wedge surface varies with distance from the tip asU = Cxmβm = 2 − βlaminar impingement flow, β = 1, the free stream velocity varieslinearly with distance from stagnation pointDetail about transformation from PDE toODE of Falkner-Skan can be found from anyFluid Mechanics textbooksyπβx
Heat transfer under free surfaceimpinging jet – Radial & Axial Velocitywithin Stagnant and Radial Wall <strong>Jet</strong>With the existence of pressure gradient, the free stream velocityis varies linearly with distance from where the flow originates(Schlichting (1968)) . In this case, the pressure gradient isattributed to the stagnation pressure created by impingement
Page 1 and 2: Free Surface Impinging JetWork done
Page 3 and 4: Introduction - Application• Verti
Page 5 and 6: Literature Review - FreeSurface Imp
Page 7: Mathematical Modelling - FreeSurfac
Page 10 and 11: Validation of laminar flow field in
Page 12 and 13: Heat transfer under free surfaceimp
Page 20 and 21: Heat transfer under partial submerg
Page 22 and 23: Heat transfer under partial submerg
Page 24 and 25: Conclusions•It was found that the
Page 26 and 27: References1. Womac, D.J., Ramadhyan
Page 28 and 29: References9. Stevens, J., Pan, Y.,

Free Surface Impinging Jet

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